The goal of this MICP (Mastering Industrial Codes and Parallelism)
was to compare the behaviours of an aft swept wing with the one of a forward swept wing
thanks to the industrial code Fluent. So two simple wings based on a NACA0012 profile
were created and studied. This study included the discovery of the usage of
Gambit to generate a profile and propagate a mesh (related in the
associated manual),
and the usage of Fluent to compute drag and lift coefficients.